US4023618A - Heat exchanger headering arrangement - Google Patents

Heat exchanger headering arrangement Download PDF

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Publication number
US4023618A
US4023618A US05/605,420 US60542075A US4023618A US 4023618 A US4023618 A US 4023618A US 60542075 A US60542075 A US 60542075A US 4023618 A US4023618 A US 4023618A
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US
United States
Prior art keywords
fluid
array
channel elements
stacked
resilient gasket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/605,420
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English (en)
Inventor
Leslie C. Kun
Kit F. Burr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Katalistiks International Inc
Honeywell UOP LLC
Original Assignee
Union Carbide Corp
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Filing date
Publication date
Priority to US05/605,420 priority Critical patent/US4023618A/en
Application filed by Union Carbide Corp filed Critical Union Carbide Corp
Priority to SE7609157A priority patent/SE7609157L/xx
Priority to DE19762637001 priority patent/DE2637001A1/de
Priority to GB34132/76A priority patent/GB1559529A/en
Priority to FR7624971A priority patent/FR2321675A1/fr
Priority to AU16901/76A priority patent/AU500378B2/en
Priority to BR7605364A priority patent/BR7605364A/pt
Priority to JP51097504A priority patent/JPS5224370A/ja
Priority to ES450773A priority patent/ES450773A1/es
Application granted granted Critical
Publication of US4023618A publication Critical patent/US4023618A/en
Assigned to MORGAN GUARANTY TRUST COMPANY OF NEW YORK, AND MORGAN BANK ( DELAWARE ) AS COLLATERAL ( AGENTS ) SEE RECORD FOR THE REMAINING ASSIGNEES. reassignment MORGAN GUARANTY TRUST COMPANY OF NEW YORK, AND MORGAN BANK ( DELAWARE ) AS COLLATERAL ( AGENTS ) SEE RECORD FOR THE REMAINING ASSIGNEES. MORTGAGE (SEE DOCUMENT FOR DETAILS). Assignors: STP CORPORATION, A CORP. OF DE.,, UNION CARBIDE AGRICULTURAL PRODUCTS CO., INC., A CORP. OF PA.,, UNION CARBIDE CORPORATION, A CORP.,, UNION CARBIDE EUROPE S.A., A SWISS CORP.
Assigned to UNION CARBIDE CORPORATION, reassignment UNION CARBIDE CORPORATION, RELEASED BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: MORGAN BANK (DELAWARE) AS COLLATERAL AGENT
Assigned to KATALISTIKS INTERNATIONAL, INC. reassignment KATALISTIKS INTERNATIONAL, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: UNION CARBIDE CORPORATION
Assigned to UOP, DES PLAINES, IL., A NY GENERAL PARTNERSHIP reassignment UOP, DES PLAINES, IL., A NY GENERAL PARTNERSHIP ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: KATALISTIKS INTERNATIONAL, INC.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/026—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • F28F9/0278—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits in the form of stacked distribution plates or perforated plates arranged over end plates
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00—Tubular elements; Assemblies of tubular elements
    • F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/14—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally
    • F28F1/16—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally the means being integral with the element, e.g. formed by extrusion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/0219—Arrangements for sealing end plates into casing or header box; Header box sub-elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/0219—Arrangements for sealing end plates into casing or header box; Header box sub-elements
    • F28F9/0224—Header boxes formed by sealing end plates into covers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/04—Arrangements for sealing elements into header boxes or end plates
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2215/00—Fins
    • F28F2215/08—Fins with openings, e.g. louvers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2230/00—Sealing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00—Fastening; Joining
    • F28F2275/20—Fastening; Joining with threaded elements
    • F28F2275/205—Fastening; Joining with threaded elements with of tie-rods
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00—Heat exchange
    • Y10S165/454—Heat exchange having side-by-side conduits structure or conduit section
    • Y10S165/471—Plural parallel conduits joined by manifold
    • Y10S165/473—Plural parallel conduits joined by manifold with clamping member at joint between header plate and header tank
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4935—Heat exchanger or boiler making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4935—Heat exchanger or boiler making
    • Y10T29/49389—Header or manifold making

Definitions

  • This invention relates to an improved headering means for a heat exchanger comprising a stacked array of thin-walled heat exchange channel elements.
  • each channel element of the heat exchanger is provided with an isostress contoured heat exchange surface comprising a multiplicity of uniformly disposed outwardly extending projections formed from a portion of each wall surface. These projections have load-bearing segments at their extremities whereby the facing walls of adjacent channel elements are mated in supportive relative with each other.
  • a substantially uniform fiber stress distribution is obtained in the isostress contoured surface. This uniform stress distribution substantially eliminates stress concentration points in the walls of the channel elements thereby permitting the walls to be fabricated from very thin sheets of thermally conductive material.
  • header means which maintain an efficient fluid-tight seal with the channel elements in the stacked array encompasses specific problems not encountered in headering arrangements in heavier walled systems.
  • channel elements having pressure withholding walls of lower thickness there is a lower resistance to heat transfer associated with the walls, in other words, a higher rate of heat transfer per unit weight of wall material, which permits the thin-walled channel elements to be closely spaced together to form a highly compact stacked array. Associated with this degree of compactness are correspondingly small dimensions for the channel elements.
  • the stacked array may be formed of 150 channel elements each 30 inches long with a cross-section characterized by a 1 inch major axis, a minor axis of 0.12 inch and a wall thickness of 0.008 inch.
  • the spacing between facing walls of adjacent channel elements may be on the order of 0.120 inch.
  • inlet header means joined in flow communication with the channel elements at one end of the array and outlet header means joined in flow communication with the channel elements at the opposite end of the array requires the fluid-tight sealing of numerous header-array joints of exceedingly small dimensions.
  • thinness of the channel element walls render them easily susceptible to bending and deformation in the heat exchanger fabrication process.
  • the tube members may be smaller in size than the openings in the tube sheet and after being passed through the openings the tubes are expanded as by swaging or other means to form a fluid-tight seal between the tubes and surrounding sheet.
  • headering arrangement which has been proposed for thin-walled channel element stacked array heat exchangers incorporates channel elements having closed ends and flat side walls at the end sections with openings in the side walls for ingress and egress of the fluid being flowed through the channel element.
  • the header means include manifold tubes passing through the openings in the channel elements, the manifold tubes having flow openings whereby fluid communication is established between the tubes and the channel elements.
  • This arrangement requires fluid-tight sealing of the numerous small joints between the tube and the associated flat side wall portions of the stacked channel elements, which is difficult to achieve economically.
  • Another variant configuration under this arrangement involves bonding of the flat side wall portions surrounding the wall openings on adjacent channel elements to each other in wall to wall contacting relationship.
  • This invention relates to an improved headering arrangement for a heat exchanger comprising a stacked array of thin-walled channel elements.
  • the invention includes a heat exchanger assembly comprising a stacked array of heat exchanger channel elements, wherein each channel element is bounded by thermally conductive pressure withholding walls of between 0.003 and 1.150 inch thickness, with a first fluid entrance opening at on end, a first fluid exit opening at the opposite end, and end sections having a cross section bounded by flat side wall portions and edge wall portions.
  • Adjacent channel elements in the array are stacked with their flat side wall portions in wall to wall contacting relationship and their edge wall portions in alignment to form a first fluid entrance face at one end of the array and a first fluid exit face at the opposite end of the array.
  • Each of the faces thus has a perimeter defined by edge wall portion ends of the stacked channel elements and side wall portion ends of the outermost channel elements in the array.
  • the pressure withholding walls of adjacent channel elements in the interior of the array are disposed in spaced relationship with respect to each other for flow of a second fluid through the array in the spaces between the channel elements in heat exchange with the first fluid.
  • Inlet header means are joined in flow communication with the first liquid entrance face for introduction of the first fluid to the channel elements, and outlet header means are joined in flow communication with the first fluid exit face for withdrawal of the first fluid from the channel elements.
  • each of the aforementioned header means comprises the improvement of a resilient gasket disposed around the perimeter of the corresponding face against the wall portion ends thereof.
  • Header tank means enclose the face, having a wall surface portion abuttingly disposed against the resilient gasket and a structurally integral flange member extending outwardly from the stacked array.
  • Means are provided joining the flange member and another structurally rigid part of the heat exchanger assembly to cause the wall surface portion of the header tank means to bear compressively against the resilient gasket for fluid-tight sealing between the header tank and the stacked array.
  • the term "resilient gasket” includes any suitable resilient or elastomeric material member which, when disposed around the perimeter of a face of the heat exchanger assembly against the wall portion ends thereof with the wall surface portion of the header tank means bearing compressively against it, is capable of providing a sealed joint which is substantilly impermeable to the fluid constituents both internal and external of the joint.
  • the resilient gasket when the aforedescribed heat exchanger assembly is employed for example as a radiator for cooling of an internal combustion engine with air as the exterior heat exchange fluid and a glycol-based aqueous solution, under pressure to prevent fluid loss and overheating, as the interior heat exchange fluid, the resilient gasket must function to maintain the interior pressure at the desired level while preventing any significant leakage of air, glycol or water through the joint between the header tank and the stacked array.
  • suitable materials for the resilient gasket may for example include materials such as Buna-N, silicone and ethylene propylene diene monomer (EPDM) elastomers and adhesive materials such as neoprene and silicone compositions.
  • EPDM ethylene propylene diene monomer
  • the specific resilient gasket may be of a type which can be preformed, e.g., provided as a unitary gasket member of the appropriate shape and size, prior to its incorporation into the heat exchanger assembly, or, alternatively, it may be of a type which is formed in situ during the fabrication of the heat exchanger assemby.
  • means are provided for joining the flange member of the header tank means and another structurally rigid part of the heat exchanger assembly to cause the wall surface portion of the header tank means to bear compressively against the resilient gasket for fluid-tight sealing.
  • structurally rigid refers to those parts of the heat exchanger assembly which, when interconnected with the flange member of the header tank means via the joining means, posses sufficient structural integrity to maintain the requisite compression for fluid-tight sealing between the header tank and the stacked array.
  • the part of the heat exchanger assembly which is associated with the joining means must be designed with sufficient moment of inertia to effectively absorb those loads, including bending and shear loads, incurred in the exertion of compression on the sealant means, without deforming or otherwise reacting in a manner which would cause loss of the fluid-tight seal.
  • the required rigidity of such associated part of the heat exchanger assembly is achieved with a low weight of material, so that a comparatively high moment of inertia is required.
  • the structurally rigid part of the heat exchanger assembly which is interconnected with the flange member of the header tank means may, in one embodiment of the invention, suitably comprise a portion of the associated end section of the stacked array.
  • the flange member of the header tank means is interconnected with a fin structure of the stacked channel element array.
  • connecting means disposed externally of the channel element stacked array interconnected corresponding portins of the structurally integral flange members, so that the aforementioned another structurally rigid part of the heat exchanger assembly for each header means comprises the structurally integral flange member of the other such headering means.
  • This embodiment has particularly utility in heat exchanger assemblies wherein the first fluid to be flowed through the channel elements is at high pressure, e.g., 60 psig, so that heavier channel element walls, as for example on the order of 0.130 to 0.150 inch thickness, are required. In such assemblies, the degree of compression required to maintain a fluid-tight seal against the high internal pressures is efficiently accommodated by mechanical connecting means joining the respective header flange members.
  • This invention is based on the discovery that resilient gaskets may advantageously be utilized to provide an effective fluid-tight joint when disposed against the end of a heat exchange channel element wall of exceedingly low thickness which forms a constituent segment of an extended perimeter around a fluid inlet or outlet face in a closely packed stacked array of channel elements.
  • the present invention employs the exceedingly small wall end surface areas of the stacked array of heat exchange channel elements as a gasketed surface without adverse loss of sealing capability even after prolonged periods of system operation.
  • a heat exchanger constructed in accordance with the invention having 0.008 inch channel element walls and suitable for as an automobile radiator may have a perimetric wall end area for gasket sealing of only 0.5 inch 2 .
  • the stacked array end sections each provide a structurally rigid matrix with a face which is buttressed by the numerous transversely extending channel element side walls; such rigid matrix possesses a relatively high mechanical strength and is able, for example, to effectively absorb bending and vibration loads which arise in the use of the heat exchanger assembly.
  • the combination of these features may account for the unexpected highly efficient performance of gasket members as sealant means in the practice of the invention.
  • the specific improvement features of the heat exchanger assembly of this invention provide a significant advantage over thin-walled heat exchangers of the prior art which required positive leak-tight sealing of numerous discrete and small sized heat exchanger core-header joints.
  • the inlet and exit faces of the heat exchanger assembly in the present invention each feature a single, extended perimeter joint surface, the fabrication of the assembly is comparatively simpler and less time-consuming and costly, relative to the thin-wall channel element heat exchanger configurations of the prior art.
  • FIG. 1 is an exploded isometric view of a part of a heat exchanger assembly according to one embodiment of the invention featuring a unitary construction header tank means.
  • FIG. 2 is an elevational view of the heat exchanger headering arrangement along line A - A of FIG. 1, as fully assembled.
  • FIG. 3 is an elevational view of a heat exchanger of the type shown in FIG. 1, as fully assembled.
  • FIG. 4 is a cross-sectional view of the heat exchanger assembly of FIG. 3 along the line B--B.
  • FIG. 5 is a sectional elevational view of a heat exchanger assembly according to another embodiment of the invention, of the shell-and-tube type.
  • FIG. 6 is an enlarged partial sectional view of the FIG. 5 heat exchanger assembly, showing the details of the headering arrangement.
  • FIG. 7 is cross-sectional view of the FIG. 6 headering arrangement along the line C--C.
  • FIG. 8 is an exploded isometric view of a heat exchanger assembly according to still another embodiment of the invention in which the flange member of the header tank means is interconnected with the fin structure of the stacked channel element array.
  • FIG. 9 is a sectional elevational view of a part of the heat exchanger headering arrangement along line D--D of FIG. 8, as fully assembled.
  • FIG. 10 is another sectional elevational view of a part of the heat exchanger headering arrangement of FIG. 8, as fully assembled.
  • FIG. 11 is an isometric view of a single heat exchange channel element such as may advantageously be used in the practice of the invention.
  • FIG. 12 an elevational view of a part of a heat exchanger assembly according to yet another embodiment of the invention featuring a formed-in-place resilient gasket.
  • FIG. 13 is an elevational view of an apparatus used to test various resilient gaskets.
  • FIG. 14 is an isometric view of a channel element stacked array such as used in the FIG. 13 testing apparatus.
  • FIG. 15 is a graph of the precent compression of the resilient gasket required for fluid-tight sealing plotted as a function of heat exchanger internal fluid pressure, for a stacked array of the type shown in FIG. 14 with various resilient gaskets.
  • FIG. 1 is an exploded partial view of an illustrative heat exchanger assembly according to the invention featuring a unitary construction header tank means.
  • the heat exchanger assembly comprises a stacked array 1 of channel elements 2.
  • Each of the channel elements is bounded by pressure withholding walls 12 of 0.008 to 0.012 inch thickness and has open ends 3 for either ingress or egress of the first fluid which is flowed through the channel elements.
  • the channel elements are each formed with end sections 4 having a cross-section bounded by flat side wall portions 5 and end wall portions 6.
  • Adjacent channel elements in the array are stacked as shown with their flat side wall portions in wall to wall contacting relationship, as indicated by reference number 7, and their edge wall portions in alignment to form a face 8 at the end of the array for either entrance or exit of the first fluid which is flowed through the channel elements.
  • This face thus has a perimeter defined by the ends 9 of the edge wall portions of the stacked channel elements and ends 10 of the outermost channel elements 11 in the array.
  • Each of the aforedescribed channel elements is constructed with a multiplicity of uniformly disposed outwardly extending projections 13 formed from a portion of pressure withholding wall surface in the interior of the array. These projections have load-bearing segments 14 at their extremities whereby the facing walls of adjacent channel elements are mated in supportive relationship with each other. In this manner the pressure force on each channel element wall is transmitted to the facing wall of the adjacent channel element.
  • the channel element surface projections are preferably of a type as disclosed and claimed in the aforementioned U.S. Pat. No. 3,757,856, incorporated herein to the extent pertinent, wherein an isostress wall surface is provided, between and surrounding the load bearing segments which is continuously curved and devoid of local mechanical loading.
  • the illustrated heat exchanger assembly further comprises structural support member 15.
  • This structural support member has a generally planar surface which is positioned against the end section of the outermost channel wall and suitable attached thereto, as for example by adhesive bonding.
  • the structural support member functions to stiffen the end sections of the outermost channel elements, thereby enhancing the structural integrity of the stacked array.
  • the headering arrangement in the FIG. 1 system includes a preformed resilient gasket 16 composed for example of silicone rubber.
  • the resilient gasket should be composed of a material having a Shore A durometer value as measured by ASTM Test No. D-2240, of between 5 and 100 and preferably between 20 and 70.
  • the durometer value is in essence a measure of the hardness of compressibility of a material, and gasket materials having durometer values in the foregoing ranges have been found particularly useful for providing fluid-tightly sealed joints in the manner of this invention.
  • all durometer values will be understood to refer to the Shore A Scale.
  • the resilient gasket with a thickness in the uncompressed state, as measured in the direction extending outwardly from the end of the channel element stacked array and generally parallel to the longitudinal axis L of the Channel elements, of between 1/32 and 1/2 inch, and a width W in the uncompressed state, as measured transversely to the outwardly extending direction, of at least 3/16 inch.
  • the resilient gasket 16 is suitably disposed around the perimeter of face 8 against the wall portions thereof so as to overlay the edge wall portion ends 9 and side wall portion ends 10 defining the perimeter.
  • Header tank means 17 are provided, comprising a tank enclosure portion 25 having U-shaped cross section defining an open tank channel 18 communicating with and enclosing the stacked array face 9 and a structurally integral flange member 20 extending outwardly from the stacked array.
  • the header tank means as shown represent a unitary construction such as may be stamped or molded as a single sheet of structural material, e.g., aluminum or plastic. It will be recognized that the tank enclosure portion 25 and the flange member 20 may be separately individually fabricated prior to the final assembly of the header tank means, but regardless of mode of fabrication, the flange member is provided as a structurally integral constituent of the header tank means.
  • the inner segment of flange member 20 adjacent the vertically disposed walls of tank enclosure portion 25 constitutes a wall surface portion 19 which is abuttingly disposed against the gasket 16.
  • suitable connection means (not shown in FIG. 1 for clarity) are provided joining the flange member, by means of the connector openings 21 therein, and another structurally rigid part of the heat exchanger assembly to cause the wall surface portion 19 of the header tank means to bear compressively against the gasket 16 for fluid-tight sealing between the header tank and the stacked array.
  • the resilient gasket sealingly engages the constituent wall portion ends 9 and 10 of the perimeter of face 8 and is held in the compressed state between the wall portion ends and wall surface portion 19 to maintain a sealed joint between the header and array.
  • the channel elements in the heat exchanger assembly are bounded by thermally conductive pressure withholding walls of between 0.003 and 0.150 inch.
  • a wall thickness of less than 0.003 inch is generally unsuitable for for channel elements due to the susceptibility of such low thicknesses to local imperfections in the material of construction which may be formed either during fabrication or in use.
  • Wall thicknesses above 0.150 inch are not suited to this invention because the heat transfer efficiency of the channel elements, as based on a unit weight of construction material, decreases with increasing wall thickness. Accordingly, maximize the heat exchange efficiency of the system, the channel element walls are characteristically designed to provide a minimum wall thickness for a given pressure differential across the channel element walls between the first and second (internal and external) fluid species.
  • channel element wall thickness in the range of 0.003 to 0.020 inch are particularly preferred in practice.
  • FIG. 2 shows an elevational view of the heat exchanger headering arrangement of FIG. 1 along line A-A, as fully assembled and with suitable connecting means joined to flange member 20.
  • the pressure withholding walls 12 of adjacent channel elements 2 in the interior of the stacked array are disposed in spaced relationships with respect to each other for flow of a second fluid through the array in the spaces 23 between the channel elements in heat exchange with the first fluid flowing through the channel elements.
  • Resilient gasket 16 is compressively positioned between the perimetric channel element wall portion ends and the wall surface portion of the flange member 20.
  • the structural support member 15 is disposed against the flat side wall portion at the end section of the outermost channel element 11 in the stacked array.
  • the wall surface portion of the header tank means is made to bear compressively against the resilient gasket by tie bar assembly 22 joining the flange member 20 and another structurally rigid part of the heat exchanger assembly.
  • FIG. 3 An elevational view of a heat exchanger of the type shown in FIG. 1 is illustrated in FIG. 3, as fully assembled.
  • the assembly of FIG. 3 is constructed and arranged for low of the second (external) fluid through the stacked array in the spaces 23 in a direction normal to the longitudinal axis L of the channel elements 2.
  • the adjacent channel elements in the array are stacked with their end section flat side wall portions bonded in wall to wall contacting relationship, as at 7.
  • Structural support members 15 are disposed against the outermost channel elements 11 in the stacked array.
  • Resilient gaskets 16 are disposed around the perimeters of the respective first fluid inlet and first fluid outlet faces against the wall portion ends thereof.
  • the header tank means 17 for this system are of the type shown in FIG.
  • each header tank means another structurally rigid part of the heat exchanger assembly comprise the several tie bar assembly mechanical connecting means 22 disposed externally of the stacked array and interconnecting corresponding portions of the flange member 20 of each of the respective header tank means.
  • the previously defined structurally rigid part of the heat exchanger assembly for each header means in this arrangement comprises the structurally integral flange member of the other header means.
  • FIG. 4 A cross-sectional view of the FIG. 3 heat exchanger assembly along the line B-B is illustrated in FIG. 4 to show the details of the headering arrangement.
  • Resilient gasket 16 is disposed around the perimeter of the stacked array between the channel element and section wall portion ends and the bearing wall surface portion of the flange member 20.
  • Tiebar assembly mechanical connecting means 22 are joined to the flange member and sidebar support member 15 is positioned against the flat side wall portion of the outermost channel element, which is stacked in wall to wall contacting relationship with the adjacent channel element at 7.
  • FIG. 5 is a sectional elevational view of a heat exchanger assembly according to another embodiment of the invention, of the shell and tube type.
  • the assembly features a cylindrical shell section 26 with second fluid inlet nozzle 27 and second fluid outlet nozzle 28.
  • the cylindrical shell section is also provided with head flanges 30 and 31 at its respective ends, whereby the shell section is joined to the first fluid inlet head section 32 featuring first fluid inlet head nozzle 33 and head flange 34 at one end and to the first fluid outlet head section 35 featuring first fluid outlet head nozzle 36 and head flange 37 at the other end.
  • the respective mating head flange pairs 30, 34 and 31, 37 may be joined by bolting or other suitable joining arrangement (not shown).
  • Each of these channel elements is bounded of thermally conductive pressure withholding walls of for example 20 mils thickness, with a first fluid opening at one end and a first fluid exit opening at the opposite end.
  • the channel elements may have a circular cross section over the intermediate sections of their length in the interior of the array, with the walls of adjacent channel elements disposed in spaced relationship with respect to each other to accommodate axial flow of the second fluid through the array in the spaces 40 between the channel elements, in heat exchange with the cocurrently flowing first fluid.
  • the end section 41 of the channel elements in the respective arrays have a cross-section bounded by flat side wall portions and edge wall portions. Adjacent channel elements in the arrays are stacked with their flat side wall portions in wall to wall contacting relationship and their edge wall portions in alignment to form a first fluid entrance face at one end of the array and a first fluid exit face at the opposite end of the array. Each such face thus has a perimeter defined by edge wall portion ends of the stacked channel elements and the side wall portion ends of the outermost channel elements in the array, as in the aforedescribed systems of FIGS. 1-4.
  • the header means in the FIG. 5 system include resilient gaskets 42 disposed around the perimeter of each face against the wall portion ends thereof, at the ends of the respective arrays.
  • the header tank means include circular plate wall members 43 vertically disposed at opposite ends of the array and having openings 44 to permit fluid flow communication between the channel elements of the stacked arrays and the inlet header plenum space 52 and the outlet header plenum space 53.
  • the outer circumferential peripheral portions of the circular plate wall members 43 thus constitute the structurally integral flange members extending outwardly from the stacked array.
  • the means joining the flange members and another structurally rigid part of the heat exchanger assembly comprise threaded tie bolts 46 having one end extending through suitable openings in extension plates 45 welded to the shell wall and secured by locking nuts 49.
  • the other ends 47 of the tie bolts pass through openings in plate wall member 43 and are secured by tightening nuts 48.
  • FIG. 6 is an enlarged partial sectional view of the first liquid inlet section of the FIG. 5 heat exchanger assembly, showing the details of the headering arrangement more clearly.
  • resilient gasket 42 is disposed around the perimeter of the inlet face of the stacked array, as formed in part by the edge wall portion ends 55 of the channel elements.
  • the edges of circular plate wall members 43 may be leak-tightly sealed against the adjacent inner surface of cylindrical shell 26 by an O-ring sealing member 56 disposed in a groove at the edge of the plate wall member.
  • the headering arrangement of FIGS. 5-6 is particularly flexible in operation, inasmuch as the degree of gasket compression required for liquid-tight sealing can be easily varied by loosening or tightening of the nuts 48 at the ends 47 of tie bolts 46, to effectively accommodate changes in operating pressure conditions.
  • FIG. 7 is a cross-sectional view of the FIG. 6 headering arrangement along the line C-C.
  • four stacked arrays are disposed in the interior of cylindrical shell section 26.
  • the channel elements in the arrays are stacked with their flat side wall portions, e.g. 58 and 59, in wall to wall contacting relationship, with the individual channel elements defining longitudinally extending first liquid flow passages 57.
  • the openings 44 in plate wall members 43 provide fluid flow communication between the channel elements of the stacked arrays and the inlet header plenum space, and gaskets 42 serve to seal the header-stacked array joints.
  • FIG. 8 is an exploded isometric view of a heat exchanger assembly according to another embodiment of the invention in which the flange member of the header tank means is interconnected with the fin structure of the stacked array of channel elements.
  • the stacked array 60 and preformed resilient gasket 64 and constructed and formed in a manner identical to that described in connection with the embodiment of FIG. 1, except tht secondary surface heat transfer fins 61 are joined to the edge wall portions of the channel elements and extend generally outwardly therefrom.
  • These secondary surface fins may suitably feature slatted louvered deformations 62 on the fin surface for added enhancement of the heat transfer.
  • the secondary surface heat transfer fins are each provided with a notch 63 in the fin surface extending from the outermost fin edge inwardly toward the channel element joined thereto.
  • the notches of the respective fins are transversely aligned with respect to the longitudinal axis L of the channel elements, preferably in a plane substantially normal to the longitudinal axis.
  • the header tank means for this system comprise an inner tank member 67, featuring structurally integral flange member segment 70 and having a plurality of spaced openings 69 therein which are disposed in fluid flow communication with the open ends of the channel elements in the stacked array 60 to provide for uniform distribution of the first fluid.
  • the portion of the inner tank member adjacent to and surrounding the series of openings 69 comprises the wall surface portion 68 which is abuttingly disposed against the resilient gasket.
  • the header tank means further comprise an outer tank member 71 having a first liquid inlet or outlet conduit 73 joined thereto and featuring structurally integral flange member segment 72.
  • the outer tank member 71 is superpositioned over inner tank member 67 as shown in FIGS. 9 and 10 to form the composite structurally integral flange member comprised of flange member segments 70 and 72.
  • the overlapping sections of the vertically disposed walls of the tank members thus extend downwardly, in the orientation shown in the drawings, over the associated end section of the stacked array.
  • FIG. 9 which is a sectional elevational view along line D-D of FIG.
  • the lower section of the vertically disposed wall of the inner tank member 67 is fitted over and positioned against the structural support member 29, which in turn is positioned against the flat side wall portion of the outermost channel element 74 in the stacked array 60.
  • the lower section of the vertically disposed wall of the inner tank member 67 also includes a portion which is fitted over and positioned against the outermost edges of the fins 61 at the associated end section of the stacked array.
  • the means joining the flange member comprises of segments 70 and 72, and another structurally rigid part of the heat exchanger assembly comprise the transversely extend plate member 65.
  • This plate member is positioned so that it extends inwardly into the notches 63 of the fins 61 and also extends outwardly beyond the outermost edges of the fins.
  • the plate member is interconnected with the composite flange member by means of an outer end segment 66 suitably crimped around an outer end segment of the flange member 70, 72 to cause the wall surface portion 68 of the header tank means to bear compressively against the resilient gasket 64 for fluid-tight sealing between the header tank and the stacked array.
  • the plate member 65 may be suitably bolted or similarly interconnected with the flange member 70, 72 to exert the requisite compression on gasket 64; in such case, the plate member crimped outer end segment 66 would not be required.
  • the another structurally rigid part of the heat exchanger assembly for the headering arrangement comprises the associated end section of the stacked array.
  • FIG. 11 is an isometric view of a single heat exchange channel element such as may advantageously be used in the practice of the invention.
  • the channel element 75 is provided with secondary surface heat transfer fins 77 and 79 which are joined to the respective edge wall portions of the channel element and extend generally outward therefrom.
  • the fins are each provided with louver type fin surface distortions, preferably of the type disclosed and claimed in U.S. Pat. No. 3,845,814, issued Nov. 5, 1974 in the name of L. C. Kun.
  • the channel element features isostress contoured wall surfaces 76 with uniformly disposed outwardly extending wall projections 81, having load-bearing segments 82 at their extremities.
  • Geometric characteristics of the channel element include a longitudinal length line K, with the cross-section of the channel element perpendicular to the longitudinal length line having a major axis maximum width line W and a minor axis F.
  • the minor axis dimension F is not a structurally measurable value, but is rather determined by dividing the measured volume of the channel element by the quantity (K x W), where the values of K and W are directly measured.
  • the widths of the respective secondary surface fins 77 and 79 are between 0.1 and 0.6 inch and each fin has a multiplicity of slotted apertures arranged in a lower configuration.
  • the adjacent slats 83 are separated by slot-shaped apertures having the fin angle ⁇ between 0° and 60° where ⁇ is the angle formed between the plane of the fin and a plane containing the maximum dimension width line W and the channel's longitudinal length line K.
  • the width of the slats 83 is between 0.82 inch and 0.10 inch and the slat angle ⁇ is between 15° and 90° where ⁇ is the angle formed between the plane of the fin and the plane of the slats.
  • the slot angle ⁇ formed between the longitudinal length line K of the channel and the longitudinal length line of the slots is between 0° and 180°.
  • Such geometry of secondary surface heat exchange fins is particularly preferred in applications where heat exchanger assemblies according to the present invention are employed as automobile heaters and radiators.
  • FIG. 12 is an elevational view of a part of a heat exchanger assembly according to yet another embodiment of the invention featuring a formed-in-place resilient gasket.
  • the gasket may suitably be fashioned in situ from either a single or a two-component adhesive composition, as for example RTV-732 silicone adhesive (single component) or XCF-3-7024 silicon adhesive (two component), products of Dow Corning Corportion, Midland, Michigan.
  • a bead of the adhesive composition is applied to the channel element wall portion ends defining the perimeter of the first fluid entrance or exit face.
  • header tank means 87 and stacked array 84 are then brought together and contacted such that the bead of adhesive forms a coherent adhesive mass 86 joining the header tank means and the stacked array, which is cured in situ to provide the resilient gasket for the system.
  • the appropriate joining means may be connected to flange member 85 and to another structurally rigid part of the heat exchanger assembly to cause the wall surface portion of the header tank means to bear compressively against gasket 85 for fluid-tight sealing between the header tank and the stacked array.
  • FIG. 13 is an elevational view of an apparatus used to test various types of resilient gaskets such as may advantageously be employed in the practice of the present invention. This apparatus was more specifically employed to determine the relationship between internal pressure in a heat exchanger assembly constructed in accordance with the invention and the degree of gasket compression required for fluid-tight sealing therein.
  • the heat exchanger test section 98 utilized in the FIG. 13 apparatus comprised a stacked array of channel elements 88, each having secondary surface heat transfer fins 89 joined to its edge wall and extending generally outwardly therefrom.
  • the test section stacked array is shown in more detail in the isometric view of FIG. 14 and was formed from 10 channel elements of aluminum construction, each having structural characteristics as generally shown in FIG. 11 with a length measured along the longitudinal length line K of 2.0 inches, with a major axis W of 0.875 inch, a minor axis F of 0.120 inch, and a wall thickness of 0.008 inch.
  • the channel elements featured in isostress surface with a multiplicity of uniformly disposed outwardly extending projections 96 formed from a portion of each wall surface and having load bearing segments 97 at their extremities whereby the facing walls of adjacent channel elements in the interior of the array were mated in supportive relationship with each other.
  • Each channel element had an end section with a cross-section bounded by flat side wall portions 99 and edge wall portions 100.
  • the adjacent channel elements in the array were stacked with their flat side wall portions in wall to wall contacting relationship and adhesively bounded together with an epoxy adhesive and thin edge wall portions in alignment to form an open face at one end of the array.
  • This face at the open end had a perimeter of 4.85 inches as defined by the edge wall portion ends 101 of the stacked channel elements and side wall portion ends 102 of the outermost channel elements in the array; the other end of the stacked array was fluid-tightly sealed closed by adhesive bonding of the array to bearing plate 90.
  • test section 98 was assembled in the test apparatus with the perimeter of its open face positioned against test gasket 92, which was in turn positioned on platform 93.
  • Platform 93 was supported on the load cell sensor 94 joined to suitable load cell means (not shown).
  • a fluid flow conduit 95 was provided as shown with an outlet section passing through an opening in platform 93 and terminating in the interior of stacked array test section 98.
  • Dial guage 91 was suitably mounted above bearing plate 90 to measure its vertical travel.
  • the lower portion of the apparatus assembly including the gasketed end of stacked array test section, was submerged in water.
  • the stacked array test section was then pressurized with air entering at elevated pressure through fluid flow conduit 95 up to a first pressure P 1 which caused bubbles to emit from the gasket joint.
  • a force F was then applied to bearing plate 90 and increased to the value F 1 at which sufficient compression was exerted to fluid-tightly seal the gasket joint, i.e., to cause cessation of the bubble emittance.
  • F 1 is the measured load cell reading at the point of fluid-tight sealing and A 1 is the area of the platform surface within the perimeter of the stacked array.
  • the term “performed gasket” refers to a gasket of the type as shown and described in connection with FIGS. 1 and 8 herein, provided as a unitary member of the appropriate shape and size.
  • formed-in-place gasket refers to a gasket of the type as shown and described in connection with FIG. 12 herein which is formed in situ during fabrication of the heat exchaner assembly.
  • non-bonded indicates that the gasket was not bonded to either the channel element wall portion ends of the stacked array or to platform 93.
  • Single-bonded denotes the systems wherein the gasket was adhesively bonded to platform 93 with a one-component silicon rubber adhesive;
  • double-boneded refers to systems wherein the resilient gasket was adhesively bonded to both the channel element wall portion ends of the stacked array and to platform 93.
  • Self-bonding characterizes the formed-in-place gasket, which develops adhesion to the channel element wall portion ends of the stacked array and to the platform 93 during its formation.
  • FIG. 15 is a graph of the percent compression of the gasket required for fluid-tight sealing, plotted as a function of the heat exchanger internal fluid pressure P 1 , in units of psig.
  • gaskets fabricated of easily compressible, low durometer material required a high level of compression for fluid-tight sealing as compared to higher durometer materials.
  • the 25 durometer silicone elastomer gasket required 85% compression for fluid-tight sealing
  • the 40 durometer nitrile (Buna-N) elastomer gasket required 61% compression
  • the 60 durometer ethylene propylene diene monomer (EPDM) elastomer required only 40% compression.
  • the FIG. 15 graph also shows that adhesive bonding of the gasket significantly reduces the amount of compression required for fluid-tight sealing.
  • the single-bonded silicone elastomer of curve 4 required 59.5% compression
  • the double-bonded silicone elastomer of curve 5 required 41% compression
  • the formed-in-place silicone adhesive gasket of curve 6 required 16% compression, at the same internal pressure P 1 of 15 psig.
  • the latter compression value, for the self-bonded formed-in-place gasket of curve 6, is particularly illustrative of the advantages of extensive bonding, inasmuch as the gasket of curve 6 requires only about 19% of the compression level which is required for fluid-tight sealing with the non-bonded gasket of curve 3 at 15 psig internal pressure. As shown in FIG.
  • the primary source of bubble emittance during the period in which the applied force on the bearing plate 90 was increased to the value F 1 required for fluid-tight sealing, was the region between the gasket 92 and the platform 93.
  • the excellent gasket sealing behavior afforded by the channel element wall portion ends has been determined to reflect a high pressure per unit area of gasket surface exerted by the channel element wall portion ends.
  • Such relative pressure levels provide for highly efficient fluid-tight sealing between the header tank and the stacked array, with the higher bearing pressures between the stacked array and the gasket surface enabling the gasket to be strongly held in place by the stacked array so that it possesses a high degree of structural stability.
  • gaskets having widths of less than 3/16 inch in the practice of the invention, due to their susceptibility to deformation and displacement by lateral forces, which can cause the gasket to roll between the respective bearing surfaces.
  • gaskets of the aforedescribed preformed type should have a thickness of between 1/32 and 1/2 inch and preferably between 1/16 and 3/16 inch.
  • the gasket thickness should not exceed 1/4 inch and preferably 1/8 inch in order to insure the formation of a void-free and homogeneous composition of the formed gasket.
  • FIG. 15 has been discussed earlier herein as illustrating the significant variation in the gasket compression required for fluid-tight sealing with respect to change in the hardness or compressibility characteristics of the gasket material, as measured by the durometer value.
  • a gasket material of less thatn 100 in order to avoid excessive compression force requirements such as are unsuitable for the thin-walled channel element stacked array.
  • gasket materials of less than 5 durometer due to their inherent susceptibility to shear and/or creep under compression. Accordingly, gasket materials of between 5 and 100 durometer are preferred in practice.
  • a heat exchanger of the type shown in FIG. 8 with channel elements of the configuration shown in FIG. 11 was constructed for use as an automobile radiator and employed with a glycol-based aqueous solution as the internal first fluid medium and air as external second fluid medium.
  • the radiator assembly was 25.0 inches wide and 18.25 inches high and comprised a stacked array of 177 channel elements, each having a major axis of 0.860 inch and a minor axis of 0.120 inch.
  • the stacked array was constructed with a spacing between adjacent channel elements in the interior of the array of approximately 0.155 inch.
  • the resilient gaskets employed in the radiator were of the preformed type, having a width of 3/8 inch and a thickness of 1/8 inch in the uncompressed state, and composed of 25 durometer silicone elastomer.
  • both sides of the gasket were coated, by knife edge application, with a thin coating of XCF3-7024 two-part silicone adhesive (XCF3-7024 silicone adhesive is manufactured by Dow Corning Corporation, Midland, Michigan);
  • the gasket was placed over the perimeter of the stacked array with the adhesive coated surface facing the header tank side of the assembly;
  • the header tank assembly was placed over the stacked array thereby securing the abutting wall portion of the header tank to the gasket by an adhesive bond;
  • the key member was positioned in keyway notches in the fin structure and the integral flange member was secured thereto to cause a 60% compression of the gasket;
  • the assembled radiator was installed in an intermediate size 1975 model automobile having a 365 cubic inch displacement V-8 engine and was road tested under highway and local driving conditions for 10,000 miles with excellent performance.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
US05/605,420 1975-08-18 1975-08-18 Heat exchanger headering arrangement Expired - Lifetime US4023618A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
US05/605,420 US4023618A (en) 1975-08-18 1975-08-18 Heat exchanger headering arrangement
ES450773A ES450773A1 (es) 1975-08-18 1976-08-17 Un conjunto de cambiador termico perfeccionado.
GB34132/76A GB1559529A (en) 1975-08-18 1976-08-17 Heat exchangers
FR7624971A FR2321675A1 (fr) 1975-08-18 1976-08-17 Collecteur perfectionne pour echangeur de chaleur
AU16901/76A AU500378B2 (en) 1975-08-18 1976-08-17 Heat exchanger headering arrangement
BR7605364A BR7605364A (pt) 1975-08-18 1976-08-17 Sistema de trocador de calor
SE7609157A SE7609157L (sv) 1975-08-18 1976-08-17 Vermevexlaranordning
DE19762637001 DE2637001A1 (de) 1975-08-18 1976-08-17 Waermeaustauscheranordnung
JP51097504A JPS5224370A (en) 1975-08-18 1976-08-17 Improved heat exchanger header structure

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JP (1) JPS5224370A (enrdf_load_stackoverflow)
AU (1) AU500378B2 (enrdf_load_stackoverflow)
BR (1) BR7605364A (enrdf_load_stackoverflow)
DE (1) DE2637001A1 (enrdf_load_stackoverflow)
ES (1) ES450773A1 (enrdf_load_stackoverflow)
FR (1) FR2321675A1 (enrdf_load_stackoverflow)
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US4191244A (en) * 1978-02-09 1980-03-04 Caterpillar Tractor Co. Modular heat exchanger with resilient mounting and sealing element
US4324290A (en) * 1979-11-12 1982-04-13 Societe Anonyme Des Usines Chausson Heat exchanger comprising a core of tubes engaged inside end plates mechanically connected with header boxes
US4331201A (en) * 1978-12-04 1982-05-25 Sueddeutsche Kuehlerfabrik Julius Fr. Behr Gmbh & Co. Kg Clamped connection
US4535839A (en) * 1982-12-20 1985-08-20 General Motors Corporation Heat exchanger with convoluted air center strip
US4550776A (en) * 1983-05-24 1985-11-05 Lu James W B Inclined radially louvered fin heat exchanger
US4637133A (en) * 1985-07-30 1987-01-20 Progressive Tool & Industries Company Apparatus for assembling radiator components
US4997035A (en) * 1990-04-02 1991-03-05 Blackstone Corporation Joint crevice corrosion inhibitor
US5257454A (en) * 1992-01-30 1993-11-02 Ford Motor Company Method of making a heat exchanger with thermal stress relieving zone
US5772958A (en) * 1994-02-18 1998-06-30 Sander Hansen A/S Method and apparatus for the pasteurization of a continuous line of products
US6527906B1 (en) * 2001-08-10 2003-03-04 Carrier Corporation Elastomer adhesive for condensing furnace heat exchanger laminate material
US20040244956A1 (en) * 2000-02-24 2004-12-09 Valeo Thermique Moteur Manifold with integrated pipe for a heat exchanger
US20050133208A1 (en) * 2003-12-19 2005-06-23 Valeo, Inc. Collar rib for heat exchanger header tanks
US20080245514A1 (en) * 2005-06-03 2008-10-09 Behr Gmbh & Co. Kg Charge Air Intercooler
WO2010066719A1 (en) * 2008-12-09 2010-06-17 BSH Bosch und Siemens Hausgeräte GmbH A condensation device for a drier
US20120097379A1 (en) * 2008-11-06 2012-04-26 Christian Riondet Collector Plate For A Heat Exchanger, And Heat Exchanger Including Such A Plate
US20130098589A1 (en) * 2011-10-21 2013-04-25 Autokuhler Gmbh & Co. Kg Manifold profile
US20140090827A1 (en) * 2012-09-29 2014-04-03 Nortiz Corporation Heat exchanger and production method thereof
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US20160377348A1 (en) * 2015-06-25 2016-12-29 Noritz Corporation Heat exchanger
US20180071022A1 (en) * 2003-07-18 2018-03-15 Covidien Lp Devices and methods for cooling microwave antennas
US20190219345A1 (en) * 2018-01-18 2019-07-18 Denso International America, Inc. Tank for heat exchanger and method for manufacturing the tank
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CN117308662A (zh) * 2023-11-27 2023-12-29 中国核动力研究设计院 一种换热器及模块式换热系统

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US4324290A (en) * 1979-11-12 1982-04-13 Societe Anonyme Des Usines Chausson Heat exchanger comprising a core of tubes engaged inside end plates mechanically connected with header boxes
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US4550776A (en) * 1983-05-24 1985-11-05 Lu James W B Inclined radially louvered fin heat exchanger
US4637133A (en) * 1985-07-30 1987-01-20 Progressive Tool & Industries Company Apparatus for assembling radiator components
US4997035A (en) * 1990-04-02 1991-03-05 Blackstone Corporation Joint crevice corrosion inhibitor
US5257454A (en) * 1992-01-30 1993-11-02 Ford Motor Company Method of making a heat exchanger with thermal stress relieving zone
US5772958A (en) * 1994-02-18 1998-06-30 Sander Hansen A/S Method and apparatus for the pasteurization of a continuous line of products
US20040244956A1 (en) * 2000-02-24 2004-12-09 Valeo Thermique Moteur Manifold with integrated pipe for a heat exchanger
US7077192B2 (en) * 2000-02-24 2006-07-18 Valeo Thermique Moteur Manifold with integrated pipe for a heat exchanger
US6527906B1 (en) * 2001-08-10 2003-03-04 Carrier Corporation Elastomer adhesive for condensing furnace heat exchanger laminate material
US20180071022A1 (en) * 2003-07-18 2018-03-15 Covidien Lp Devices and methods for cooling microwave antennas
US8181694B2 (en) 2003-12-19 2012-05-22 Valeo, Inc. Collar rib for heat exchanger header tanks
US20070261835A1 (en) * 2003-12-19 2007-11-15 Michael Powers Collar Rib for Heat Exchanger Headers Tanks
US20050133208A1 (en) * 2003-12-19 2005-06-23 Valeo, Inc. Collar rib for heat exchanger header tanks
US9046311B2 (en) * 2003-12-19 2015-06-02 Valeo, Inc. Collar ribs for heat exchanger headers tanks
US20080245514A1 (en) * 2005-06-03 2008-10-09 Behr Gmbh & Co. Kg Charge Air Intercooler
US20120097379A1 (en) * 2008-11-06 2012-04-26 Christian Riondet Collector Plate For A Heat Exchanger, And Heat Exchanger Including Such A Plate
US9297594B2 (en) * 2008-11-06 2016-03-29 Valeo Systemes Thermiques Collector plate for a heat exchanger, and heat exchanger including such a plate
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AU1690176A (en) 1978-02-23
GB1559529A (en) 1980-01-23
JPS5427576B2 (enrdf_load_stackoverflow) 1979-09-11
AU500378B2 (en) 1979-05-17
BR7605364A (pt) 1977-08-16
ES450773A1 (es) 1977-12-16
FR2321675A1 (fr) 1977-03-18
JPS5224370A (en) 1977-02-23
SE7609157L (sv) 1977-02-19
DE2637001A1 (de) 1977-02-24

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